A study of low-thrust guidance.
Formulation of problem of guiding low thrust spacecraft back to nominal trajectory
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Formulation of problem of guiding low thrust spacecraft back to nominal trajectory
Vehicle mass requirements for optimal high and low thrust propulsion systems for manned and unmanned planetary missions
Electrostatic ion thrustor employing cesium on tungsten contact ionization for satellite attitude control and stationkeeping missions
Trajectory optimization problems in mechanics of low thrust propulsion for solar sail and power limited space flights
Approximate analytic solution for variables describing three dimensional solar powered heliocentric low thrust trajectory in vicinity of ecliptic plane
Constant thrust electric propulsion systems performance with coast trajectories presented for 1.0 AU extraecliptic missions
Solar electric low thrust propulsion application to Jupiter swingby mission to outer planets
Precision flow measurement techniques for low thrust auxiliary propulsion liquid rockets
Current computer programs for low thrust trajectory analysis using flyby and rendevous trajectories
Spacecraft optimum low thrust trajectory analyzed by Hamilton-Jacobi perturbation theory, obtaining canonic constants of motion
Low thrust mission simulation dependence on hardware definition, discussing power plant characteristics, jet velocity and thrustor efficiency
Interplanetary low thrust mission analysis model, discussing major elements interactions
Low thrust mission analysis techniques and computer programs, discussing electric propulsion
Low thrust trajectories for minimum time rendezvous between continuous thrust interceptor and passive target vehicle, comparing calculus of variations and steepest ascent analyses
Low thrust reaction control for space missions, summarizing range and specific impulse characteristics for solid and hybrid systems
Recurrent Lagrange multipliers for optimal low thrust earth-Jupiter transfers, using three dimensional solar system model
Low thrust mission analysis and computer programs
Optimum low thrust ion propelled interplanetary trajectory design using two step Chebyshev method